Fuzzy optimized control based on T-S model for satellite attitude control system to reduce limit cycle
Keyword(s):
2013 ◽
Vol 46
(20)
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pp. 456-461
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1972 ◽
Vol 17
(4)
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pp. 526-528
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1983 ◽
Vol 16
(11)
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pp. 575-582
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2006 ◽
Vol 27
(2)
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pp. 125-140
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2020 ◽
Vol 357
(4)
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pp. 2354-2370